Investigation, at Inlet Locations, of Fuselage Flow Fields at Transonic and Supersonic Speeds PDF Download
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Author: Lyndell S. King Publisher: ISBN: Category : Aerodynamics, Supersonic Languages : en Pages : 132
Book Description
Wind tunnel tests were conducted to determine the flow distribution about fuselage configurations at transonic and supersonic speeds and at angles of attack up to 20 degrees. The models tested were approximately one-twelfth scale and consisted of a main fuselage forebody member and several attachable components. The components were mounted in several combinations to represent different possible configurations for tactical aircraft. Flow distribution surveys were conducted at two inlet locations ahead of and under the wing to assess the effects of forebody geometry for the conditions indicated. The data indicate the influence of the canopy, nose droop, and fuselage shape on flow angularities in the forward survey plane.
Author: Lyndell S. King Publisher: ISBN: Category : Aerodynamics, Supersonic Languages : en Pages : 132
Book Description
Wind tunnel tests were conducted to determine the flow distribution about fuselage configurations at transonic and supersonic speeds and at angles of attack up to 20 degrees. The models tested were approximately one-twelfth scale and consisted of a main fuselage forebody member and several attachable components. The components were mounted in several combinations to represent different possible configurations for tactical aircraft. Flow distribution surveys were conducted at two inlet locations ahead of and under the wing to assess the effects of forebody geometry for the conditions indicated. The data indicate the influence of the canopy, nose droop, and fuselage shape on flow angularities in the forward survey plane.
Author: Publisher: ISBN: Category : Aeronautics Languages : en Pages : 896
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author: Lyndell S. King
Author: Lyndell S. King
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Author: United States. Superintendent of Documents
Author: United States. Superintendent of Documents
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